National Aerospace Laboratory
Fujitsu Limited
Daiko Limited
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory SP-14
巻
14
ページ
49 - 52
発行年
1990-11
抄録（英）
The "rarefied gas numerical wind tunnel" constructed on the National Aerospace Laboratory Numerical Simulator System with the universal code described using the null-collision direct-simulation Monte Carlo method is used for the simulation of rarefied gas flows around a flat-plate delta wing at a large angle of attack. Some flowfield properties shown by computer graphics are presented.
希薄気体数値風洞 VI. デルタ翼
nalsp0014008.pdf
(1.12MB)
